View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 67694U 26145.33548020 +.00000000 +00000-0 +72734-3 0 00004
2 67694 97.2845 256.8675 0000828 89.4527 270.6810 15.33455186 06
| Epoch (UTC): | 25 May 2026 08:03:05 |
| Eccentricity: | 0.0000828 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.8675° |
| argument of perigee: | 89.4527° |
| revolutions per day: | 15.33455186 |
| mean anomaly at epoch: | 270.6810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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